Price Quote Get an up to date pricing and availability quote for this product. Order online or over the phone.
Quality Commitment
Serving our customers with quality and safety first.
- AS9120 Certified
- Audited supply chain
- ITAR Registered
- DDTC Registered
- HAZMAT Certified
- Customer service objectives
- Every product 100% inspected
Datasheet. 1853M33P06 specification
The national stock number or the identification information of the end equipment for which the item is a part.
ecu/eec, NON-Pmux (737 aew and c engine)
The name assigned to the item by the government agency or commercial organization controlling the design of the item.
control UNIT-Electronic
Answers.
Schedule B number: 8411997050
Parts of gas turbine aircraft engines, other than for use in civil aircraft
FSC 2995 ⁓ Miscellaneous engine accessories, aircraft
Note-items classified in this class must be specifically designed for use with aircraft or quided missile primemovers only.
Excluding exhaust system; (fsc 1560); jet engine hydraulic reservoirs (fsc 2840); jet engine oil tanks (fsc 2840); electrical starters (fsc 2925); cockpit mounted control quadrants (fsc 1680); aircraft engine covers (fsc 1730).
NSN 2995-01-621-1956 CONTROL UNIT,SUPERVISORY,TURBINE
Used on ecu/eec, non-pmux (737 aew and c engine). control unit-electronic
- NIIN
- 016211956
- NIIN Date
- 08/27/13
- Schedule B
- 8411997050
- Name Code
- 47093
- FIIG
- A23900
- DEMIL / ITAR
- Uncontrolled item (Code )
- Hazmat
- No hazard information available from HMIRS.
- MSDS
- N/A
- Precious Metals
- --
- Enviromental
- N/A
- Electrostatic ESD & EMI
- No ESD or EMI sensitivity
Major End Users Countries and entities
- - Australia
- - Republic of Korea
- - Nato Maintenance And Supply Agency
Availability for 1853M33P06 A member of our team will provide you with a price and availability quote
Request a Quote »Similar by Design Other control units with similar characteristics
Nothing similar to this part number was found in our inventory
1853M33P06 / Control unit,supervisory,turbineWhat is the formal definition of this item?
An electronic unit that continously monitors engine speed, temperature, and air flow and adjusts the fuel control, main, turbine engine to compensate for changes. features may include load sharing capabilities, rotor speed governing, loss-of-load protection and analog or manual backup modes. it may contain automatic start capability or self-diagnostic circuitry.
